Publication Date:
2019-08-17
Description:
Design data are presented for the graphical construction of two-dimensional sharp-edge-throat supersonic nozzles of minimum length for test-section Mach numbers from 1.20 to 10.00. The method of characteristics used in the design is briefly reviewed.
Keywords:
Aircraft Design, Testing and Performance
Type:
NACA-RM-E8J12
Format:
application/pdf
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